SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 FG36

2015 FG36

2015 FG36 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.1 AU it takes 1.15 yr to circle the Sun.

Apollo Observations: 81
Orbital Period · P
1.15 yr
v(q)
33.7 km/s
v(Q)
24 km/s
Diameter · ≈
0.06 km
TJ
5.64
Eccentricity · e
0.1685

Orbit and dynamics

The path is an ellipse reaching 0.915 AU from the Sun at perihelion and 1.285 AU at aphelion, a radial span of 0.37 AU.

Applying Kepler's third law to a = 1.1 AU gives an orbital period of 1.15 yr, or about 421 days.

An eccentricity of 0.169 makes the orbit moderately elongated.

Its inclination of 3.51° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.7 km/s at perihelion and falls to 24 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.82 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 81 observations and has a weighted RMS residual of 0.4905 arcseconds.

Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
1.1 AU
Eccentricity
0.1685
Perihelion
0.915 AU
Aphelion
1.28535 AU
Inclination
3.51°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
188.65°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2030-Apr-19 08:28 0.075197 AU
11249246 km
3.63 km/s
2030-Nov-06 00:17 0.255293 AU
38191224 km
5.03 km/s
2037-Mar-21 19:55 0.382510 AU
57222625 km
16.43 km/s
2038-Jan-01 23:00 0.303959 AU
45471601 km
6.37 km/s
2038-Sep-14 10:52 0.209623 AU
31359124 km
11.37 km/s
2045-Mar-10 18:06 0.167587 AU
25070629 km
3.54 km/s
2045-Jun-14 02:35 0.113119 AU
16922404 km
4.41 km/s
2045-Oct-15 00:38 0.207710 AU
31072990 km
3.81 km/s
2052-Mar-26 17:16 0.264845 AU
39620202 km
12.91 km/s
2052-Dec-18 05:12 0.308410 AU
46137490 km
6.38 km/s
2053-Sep-19 18:55 0.329730 AU
49326864 km
14.90 km/s
2060-Feb-13 00:38 0.232015 AU
34709005 km
5.01 km/s
2060-Aug-02 10:51 0.081252 AU
12155174 km
4.05 km/s
2067-Mar-31 03:38 0.176134 AU
26349328 km
10.21 km/s
2067-Dec-08 06:00 0.302757 AU
45291822 km
6.22 km/s
2068-Sep-23 05:10 0.410743 AU
61446263 km
17.28 km/s
2075-Feb-06 00:22 0.247052 AU
36958385 km
5.33 km/s
2075-Aug-19 21:04 0.052351 AU
7831630 km
4.15 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
23.82

Orbit Quality

RMS
0.49051
Condition
0
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

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